Unmanned aerial vehicle navigation decoy system
A technology of unmanned aerial vehicle and remote control system, which is applied in radio wave measurement system, satellite radio beacon positioning system, traffic control system, etc. The effect of stable operation and guarantee of operation safety
Pending Publication Date: 2021-03-19
中交遥感天域科技江苏有限公司
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Problems solved by technology
[0002] Existing drone navigation deception includes traction navigation deception signal generation system, star search system, drone flight direction deception remote control system and antenna array. The drone flight direction deception remote control system is also called black flight in the industry. The flying direction of the UAV is used to deceive the remote control system. The antenna array is generally protected by a radome. Due to the design defects of the structure and shape of the existing antenna shield, it is prone to a series of problems such as large wind resistance and water accumulation, which greatly reduces the radome. protective performance
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[0019] The present invention will be further described below in conjunction with the accompanying drawings.
[0020] as attached figure 1 As shown, the UAV navigation deception system includes a towed navigation deception signal generation system 1, a satellite search system 2 connected to the towed navigation deception signal generation system 1, a UAV flight direction deception remote control system 3 and an antenna array 4. The decoy principle is: the star search system 2 analyzes the real satellite signal after receiving it, and transmits the analyzed result data to the traction navigation deception signal generation system 1, and at the same time transmits the analyzed result data to the UAV flight direction to deceive the remote control System 3 processes, UAV flight direction deception remote control system 3 starts traction navigation deception signal generation system 1, and simultaneously controls the supporting display screen to display corresponding instruction inf...
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The invention discloses an unmanned aerial vehicle navigation decoy system. The system comprises a pull-type navigation deception signal generation system, and a satellite searching system, an unmanned aerial vehicle flight direction decoy remote control system and an antenna array which are in communication connection with the pull-type navigation deception signal generation system; the system further comprises a base station platform and an antenna protective cover, the pull-type navigation deception signal generation system, the satellite searching system, the unmanned aerial vehicle flightdirection decoy remote control system and the antenna array are all arranged on the base station platform, the antenna protective cover covers the antenna array, and the antenna protective cover is of a dome and cylinder body assembly structure. The unmanned aerial vehicle navigation decoy system provided by the invention can perform navigation decoy on a black-flying unmanned aerial vehicle to take over and control the black-flying unmanned aerial vehicle, and the device is stable and reliable in operation.
Description
technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle navigation decoy system. Background technique [0002] Existing drone navigation deception includes traction navigation deception signal generation system, star search system, drone flight direction deception remote control system and antenna array. The drone flight direction deception remote control system is also called black flight in the industry. The flying direction of the UAV is used to deceive the remote control system. The antenna array is generally protected by a radome. Due to the design defects of the structure and shape of the existing antenna shield, it is prone to a series of problems such as large wind resistance and water accumulation, which greatly reduces the radome. protection performance. Contents of the invention [0003] Purpose of the invention: In order to overcome the deficiencies in the prior art, the prese...
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Login to View More IPC IPC(8): G01S19/14G01S19/21G05D1/10G08G5/00
CPCG01S19/14G01S19/21G05D1/101G08G5/0095
Inventor 苏颖闫廷廷嵇强翟智云
Owner 中交遥感天域科技江苏有限公司